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WO/2012/170980 |
Described are passenger seat assemblies having at least one seat back support and at least one seat pan coupled to the at least one seat back support. The passenger seat assemblies may also include at least one pair of armrests coupled t...
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WO/2012/168741 |
The invention provides an extendible member (10) which is configurable between a coiled form (11) and an extended form (12). The extendible member (10) comprises: a primary member (14) comprising a sheet of material resiliently biased in...
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WO/2012/170198 |
There is provided an insulation system (100) and method for a trans¬ port vehicle (10). The system has first (106a) and second (106b) frame members; a first rigid foam insulation member (124a) extend¬ ing between the first (106a) and s...
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WO/2012/170672 |
According to various embodiments, apparatuses and methods for providing a control system for aircraft refueling trucks is provided. The control system is configured for facilitating remote troubleshooting of one or more safety mechanisms...
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WO/2012/171034 |
The spiroid wing tip according to embodiments of the invention including a continuous segmental assembly having a closed loop frontal profile comprising a lower near vertical segment, a horizontal segment, a vertical segment, a second ho...
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WO/2012/169906 |
A composite structure forming a load bearing composite shell for a helicopter, with a shell which defines the exterior of a fuselage and includes a central fuselage section and tail boom, a fuselage which is adapted house an engine or dr...
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WO/2012/170404 |
A mounting system (50) and method capable of reducing backbone deflection in a high-bypass turbofan engine (10). The system (50) includes a rigid structure (54) and a linkage mechanism having at least first and second links (62, 64, 66) ...
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WO/2012/171004 |
Methods and devices are described for reducing the torque and the level of vibration on a helicopter rotor blade by maintaining a constant lift and constant (low) drag on each section of the blade throughout the entire revolution. A roto...
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WO/2012/170668 |
A high- strength, lightweight inflatable structure (10) is formed of at least one flexible fabric member (24, 26) that, in an inflated condition, forms a self-supporting structure. The flexible fabric member (24, 26) is formed from a bar...
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WO/2012/168881 |
Described is a radio-controlled helicopter (1) comprising a main body (2), a tail beam (3), connecting means (25, 29, 35, 36, 37, 38) operating between the main body (2) and the tail beam (3) for connecting the tail beam (3) to the main ...
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WO/2012/170980 |
Described are passenger seat assemblies (10) having at least one seat back support (12) and at least one seat pan (14) coupled to the at least one seat back support (12). The passenger seat assemblies (10) may also include at least one p...
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WO/2012/170956 |
A hollow fiber fluid separation device lOOg includes a hollow fiber cartridge 11, comprising a plurality of hollow fiber membranes arranged around a central tubular core 15, a first tubesheet 17a and a second tubesheet 17b encapsulating ...
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WO/2012/170933 |
A hollow fiber device (11) includes a hollow fiber bundle (13), comprising a plurality of hollow fibers, a first tubesheet (17a) and a second tubesheet (17b) encapsulating respective distal ends of the hollow fiber bundle. The tubesheets...
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WO/2012/167769 |
A device for reducing structural vibrations of aerofoils in an aircraft comprises, in the region of the aerofoil tips, at least one force generator (24a) acting substantially in the direction of movement of the vibrations. This arrangeme...
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WO/2012/164187 |
The invention relates to an air inlet structure (100) for a turbojet engine nacelle, comprising: (i) at least one stationary internal wall (41) intended to be attached to at least one element (20) of a mid-section (2) of the nacelle, and...
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WO/2012/164708 |
In order to enable a worker who loads and unloads cargo into and from an aircraft to grasp the inclination state of a fuselage to thereby prevent fuselage pratfall accident and nose landing gear breakage accident and achieve a smooth ope...
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WO/2012/165887 |
The present invention pertains to a technique for supplying power to an object in midair, and more specifically, to a ground-level power supply system for a small unmanned aerial robot to continuously supply power as a power source for t...
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WO/2012/163512 |
The invention relates to an aircraft including a cabin and a door panel (6) comprising, facing the lintel (5) of the opening (3), a sealing strip (13) having a heel piece (14) secured to the internal face of the door panel (6) and a flex...
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WO/2012/165887 |
The present invention pertains to a technique for supplying power to an object in midair, and more specifically, to a ground-level power supply system for a small unmanned aerial robot to continuously supply power as a power source for t...
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WO/2012/165042 |
The present invention enables an actuator drive motor at which an anomaly such as failure has occurred to be halted/arrested in a shorter period of time without adopting a mechanical brake mechanism. The present invention is an electric ...
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WO/2012/164197 |
The invention relates to an assembly for an aircraft nacelle, characterized in that it includes: a flange (30) comprising at least one first portion (31) to be attached to another flange, and a second portion (32) which extends transvers...
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WO/2012/165043 |
The present invention enables greater compactness and lightweightness in addition to being able to be applied to transient, large, instantaneous current arising during electric actuator acceleration. The present invention is an electric ...
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WO/2012/163513 |
The invention relates to an emergency opening device for an aircraft door provided with an opening mechanism (10, 11, 17), said device comprising (i) a mobile manoeuvring member (21-23, 35) urged by elastic compression means (20) and pro...
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WO/2012/164186 |
The invention relates to a nacelle (1) for an aircraft bypass turbojet engine (6), comprising downstream: an internal stationary structure (8) intended to surround part of the bypass turbojet engine (6); and an external structure (9) at ...
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WO/2012/162910 |
An aviation recorder submarine search device and a method thereof are provided. The device comprises a black box (1), and the black box (1) is set in an ejection tube device (2), and a first cabin door (3) is set on one side of the eject...
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WO/2012/164391 |
Described are passenger seats including a lower frame (16) comprising a pair of supports (40), a seat pan (12) adjustably coupled to the pair of supports via a coupling system, and a rear leg (18) coupled to the lower frame, wherein the ...
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WO/2012/163538 |
The invention relates to an aircraft gas-turbine engine with an engine lining (29) which surrounds a core engine (30) in a tubular manner, characterized in that at least one inflow-side part (30) of the engine lining (29) is displaceable...
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WO/2012/163325 |
The invention relates to a method for producing a surface structure (30) with a lightning protection device (31) having the following steps: a) provision of a carrying structure (34) on the basis of a fibre composite material, b) applica...
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WO/2012/164214 |
A system for conditioning the air of a passenger compartment (1) of an aircraft, the system comprising an air supply circuit connecting at least one exterior air inlet (E) to at least one air distribution outlet (S) opening into the comp...
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WO/2012/162444 |
A compact in-wheel vehicle motor and gearing system designed to meet high power and torque requirements for driving a vehicle on the ground independently of other power sources is provided. The motor and gearing system includes a motor a...
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WO/2012/160443 |
Embodiments of the present invention provide an improved pivot articulation for a kinematic seat. Certain embodiments provide an elastic pivot that is formed as flexion weaves that connect upper and lower portions of a seat back.. The fl...
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WO/2012/162381 |
Methods, apparatuses and articles of manufacture to provide passenger preference data to in-flight entertainment systems are disclosed. A disclosed example airline passenger seat includes an optical device to optically scan a barcode pre...
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WO/2012/160375 |
An air vehicle powered by a gas turbine engine, particularly, but not exclusively, an air vehicle having a blended wing body comprises a gas turbine engine disposed in the body of the vehicle including an inlet face. An inlet channel hav...
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WO/2012/160111 |
Embodiments of the present invention relate to a rocket or ballistic launch rotary wing air vehicle.
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WO/2012/159386 |
Disclosed is a incline cyclic pitch and collective pitch control mechanism. The incline cyclic pitch and collective pitch control mechanism includes a fixing seat (27), a servo device (4) arranged on the fixing seat (27), a swashplate (1...
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WO/2012/160581 |
The present invention concerns a seating unit (1), in particular for aircrafts' economy class, comprising a substantially rigid fixed shell (4), a support structure (9), a backrest (2) and a seat (3), all contained within said shell (4),...
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WO/2012/159735 |
The invention relates to a seat fastening device for fastening a seat or for lashing loads to at least one fastening rail (82) that is fastened to a floor (80), having a main body (10), a longitudinal fastening unit (36) having at least ...
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WO/2012/161608 |
The group of inventions relates to aircraft and watercraft, and also to signalling devices. The method for preventing flow separation over the wing of an aerohydrodynamic device consists in that, during movement of the wing, a wing part ...
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WO/2012/161680 |
A blade-pitch control system for controlling a pitch angle of blades on a rotor has an input swashplate assembly having non-rotating and rotating portions, the rotating portion being operably connected to blade grips. A feedback swashpla...
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WO/2012/161929 |
A ram air turbine (32) comprises a turbine housing (72) which mounts a number of circumferentially spaced turbine blades (104) that function predominantly as impulse turbine blades and a number of splitters (106), each located in between...
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WO/2012/159890 |
An arrangement (2) for generating and treating water comprises a fuel cell (4) with a water- generating system, a salination unit (14) for the salination of water, a state measuring device (16) for acquiring an operating state of the sal...
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WO/2012/161630 |
The present invention relates to a method for steering a UAV, Unmanned Aerial Vehicle, to enable a high level command of the UAV. The method comprising the steps of: determining (500) a reference position (200, 300, 400) related to a pos...
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WO/2012/160111 |
Embodiments of the present invention relate to a rocket or ballistic launch rotary wing air vehicle.
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WO/2012/159608 |
In order to create a lightweight, effective, cheaply producible ice protection device for deicing an aircraft and/or for keeping the aircraft free from ice, the invention creates a composite structure (10) for an aircraft component (42) ...
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WO/2012/161925 |
Embodiments of the present invention provide a system that provides a cohesive, harmonized look to aircraft galleys and other aircraft areas. The system allows airlines to easily change the decorative front fascia of galley (and other) a...
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WO/2012/156654 |
The invention relates to a device (1) for reducing jet lag, configured such as to be built into an aircraft (2), said device (1) being characterised by including: a set of sensory stimulators (4) including at least one light-emitting sou...
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WO/2012/155873 |
A movable access or loading device (1) for an aircraft (2) with a scanner (10) arranged on the access or loading device, wherein the position of the aircraft (2) relative to the axis or loading device (1) is determined by the scanner (10...
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WO/2012/158067 |
The invention relates to the field of aircraft engineering and, more specifically, to vertical take-off and landing aircraft. The aircraft comprises a body having a round or elliptical shape with a convex upper surface and a flat lower s...
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WO/2012/159056 |
Generally, an inventive aircraft (1) having at least a first lift body (2) and a second lift body (3) each controllably configurable to correspondingly generate an amount of lift (4) sufficient to remain aloft at a first elevation (5) an...
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WO/2012/155418 |
A side rod control device (10) with three degrees of freedom is provided with a pitch control mechanism (300), a roll control mechanism (400) and a front wheel turning control mechanism (200) which are arranged along three mutually verti...
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